In-plane/out-of-plane librations of a tethered system in elliptical orbits

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 44, Issue 142, 2001, Pages 196-202

  Takeichi, N ^a   Natori, M C ^a   Okuizumi, N ^a  

^a UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; DRAG; EQUATIONS OF MOTION; LAGRANGE MULTIPLIERS; MATHEMATICAL MODELS; MATRIX ALGEBRA; NUMERICAL ANALYSIS; ORBITS; TETHERLINES;

ATMOSPHERIC DRAG; ELLIPTICAL ORBITS; LIBRATION; LONGITUDINAL ELONGATION; ORBITAL MOTION; TETHERED SYSTEM;

SATELLITES;

EID: 0035246270     PISSN: 05493811     EISSN: None     Source Type: Journal    
DOI: 10.2322/tjsass.43.196     Document Type: Article

References (14)

1. Feasibility study on a tethered satellite system
2. Dynamic behaviour of a tethered system with multi-sub-satellite in elliptic orbits
3. Periodic solutions associated with the gravity-gradient-oriented system: Part I. Analytical and numerical determination
4. Periodic solutions associated with the gravity-gradient-oriented system: Part II. Stability analysis
5. Chaos in the pitch equation of motion for the gravity-gradient satellite
6. Numerical investigation of chaos in the attitude motion of a gravity-gradient satellite
7. Nonlinear dynamics of two-body tethered satellite systems
8. Nonlinear dynamics of the tethered system in the station keeping phase
9. Dynamics of the orbital cable system
10. Tethered satellite swinging from atmospheric gradient
11. Dynamics of a tethered satellite subjected to aerodynamic forces
12. Dynamics of a tethered satellite in elliptic, non-equatorial orbits